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DEVICE FOR EMERGENCY OPENING OF AN AIRCRAFT DOOR, WITH LEVER RETAINER

机译:带有杠杆固定器的紧急打开飞机门的装置

摘要

Device for emergency opening of an aircraft door provided with an opening mechanism, comprising: - actuation means (2, 5) of the opening mechanism comprising: a tubular operating member (2 ) and a second locking end (4) which has a stop surface (43); elastic compression means (5); a retaining member for the second locking end (4), the retaining member comprising a rotary latch (9) and a lever (44) adapted to cooperate with the stop surface (43), the rotary latch (9 ) being rotatable about the axis of movement of the operating member (2); -activation means (31) actuation means (2, 5) adapted to drive the rotary lock (9).
机译:用于紧急打开飞机门的装置,其具有打开机构,包括:-打开机构的致动装置(2、5),包括:管状操作构件(2)和具有止动表面的第二锁定端(4) (43);弹性压缩装置(5);用于第二锁定端(4)的保持构件,该保持构件包括旋转闩锁(9)和适于与止动表面(43)配合的杠杆(44),该旋转闩锁(9)可绕轴线旋转操作部件(2)的运动; -致动装置(31),致动装置(2、5),其适于驱动旋转锁(9)。

著录项

  • 公开/公告号FR3084334A1

    专利类型

  • 公开/公告日2020-01-31

    原文格式PDF

  • 申请/专利权人 LATECOERE;

    申请/专利号FR1856874

  • 发明设计人 DIDIER MOLINARI;

    申请日2018-07-24

  • 分类号B64C1/14;B64D25;

  • 国家 FR

  • 入库时间 2022-08-21 11:00:33

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